US7845085B2 - Identifying a directional reference using rate gyros oriented along different axes - Google Patents
Identifying a directional reference using rate gyros oriented along different axes Download PDFInfo
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- US7845085B2 US7845085B2 US11/777,072 US77707207A US7845085B2 US 7845085 B2 US7845085 B2 US 7845085B2 US 77707207 A US77707207 A US 77707207A US 7845085 B2 US7845085 B2 US 7845085B2
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- G—PHYSICS
- G08—SIGNALLING
- G08C—TRANSMISSION SYSTEMS FOR MEASURED VALUES, CONTROL OR SIMILAR SIGNALS
- G08C21/00—Systems for transmitting the position of an object with respect to a predetermined reference system, e.g. tele-autographic system
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C19/00—Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C19/00—Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
- G01C19/02—Rotary gyroscopes
- G01C19/34—Rotary gyroscopes for indicating a direction in the horizontal plane, e.g. directional gyroscopes
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C19/00—Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
- G01C19/56—Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces
Definitions
- ground sensors typically monitor an area of coverage, and report activity to a central location.
- Some conventional unmanned ground sensors are constructed so that they can be dropped from the air across a region of potentially hostile activity.
- unmanned ground sensors In contrast to manned vehicles which can employ expensive and mechanically complex gyroscopic compasses to facilitate navigation, unmanned ground sensors must be relatively small, durable and reliable since it is unlikely that the unmanned ground sensors individually can be conveniently retrieved and repaired. Rather, such unmanned ground sensors are typically distributed at stationary locations in the field in a sacrificial manner (i.e., with little or no intention of recovering and reusing the ground sensors due to hostile surroundings). Accordingly, such sensors are typically simple, low cost, remotely operational units.
- One conventional unmanned ground sensor is equipped with an electronic magnetic compass that enables the ground sensor to determine the direction of the earth's magnetic north pole.
- the ground sensor is further equipped with a sensor assembly that detects activity in the vicinity of the ground sensor (e.g., general seismic activity, vehicle movement, human activity, etc.). When the ground sensor detects such activity, the ground sensor transmits data conveying the direction of that activity relative to the earth's magnetic north pole.
- the electronic magnetic compasses used by the conventional ground sensors are extremely sensitive to environmental influences such as temperature and magnetic interference.
- field disturbances due to neighboring iron deposits and/or current loops e.g., from wells, manholes and sewer caps, pipes, buildings, towers, etc.
- an improved technique of identifying a directional reference utilizes rate gyros.
- the angular rate sensing capabilities of rate gyros make the rate gyros generally insensitive to levelness and magnetic interference. Rather, the rate gyros provide signals along particular sensing axes (X, Y, and Z axes) which, when vector summed, enable identification of the earth's true north direction. As a result, there is no need to convert magnetic north data to true north data. Moreover, influences such as levelness, temperature, local magnetic field disturbances are unlikely to significantly interfere with the operation of the rate gyros.
- One embodiment is directed to a deployable stationary device which includes (i) a device support, (ii) rate gyros supported by the device support, the rate gyros being oriented along different axes, and (iii) a controller supported by the device support.
- the controller is arranged to receive rate gyro signals from the rate gyros. Each rate gyro signal indicates a rate of rotation about a respective axis associated with a particular rate gyro.
- the controller is further arranged to perform a vector sum operation based on the rate gyro signals, and generate a direction signal which identifies a direction resulting from performance of the vector summing operation.
- Such a deployable stationary device is capable of operating as one of a network of such devices in a surveillance system to enable detection and precise location of suspicious activity.
- FIG. 1 is a general diagram of a deployable stationary device which utilizes rate gyros to determine true north.
- FIG. 2 is a general diagram of a surveillance system which utilizes multiple deployable stationary devices.
- FIG. 3 is a flow diagram illustrating particular operations of the surveillance system of FIG. 2 .
- FIG. 4 is a flowchart of a procedure performed by the deployable stationary device of FIG. 1 .
- rate gyros An improved technique of identifying a directional reference utilizes rate gyros.
- the angular rate sensing capabilities of rate gyros generally make the rate gyros insensitive to levelness and magnetic interference. Rather, the rate gyros provide signals along particular sensing axes (X, Y, and Z axes) which, when vector summed, enable identification of the earth's true north direction. Accordingly, there is no need to convert magnetic north data to true north data. Furthermore, influences such as levelness, temperature, local magnetic field disturbances are unlikely to significantly interfere with the operation of the rate gyros.
- FIG. 1 is a general diagram of a deployable stationary device 20 which carries out angular rate sensing along multiple axes to determine true north.
- the deployable stationary device 20 includes a device support 22 , sensors 24 (A), 24 (B), 24 (C), . . . (collectively sensors 24 ), multiple rate gyros 26 , a controller 28 , a communications interface 30 , and a power supply 32 .
- the device support 22 is a rugged enclosure which robustly and reliably supports the other components (e.g., the sensors 24 , the rate gyros 26 , the controller 28 , etc.) for deployment in the field (e.g., via an air drop, manual installation, via an unmanned vehicle, etc.). Once the deployable stationary device 20 reaches its stationary destination, the device support 22 protects these components from environmental influences at the stationary destination (e.g., against poor whether conditions).
- the other components e.g., the sensors 24 , the rate gyros 26 , the controller 28 , etc.
- the sensors 24 electrically connect to the power supply 32 for power, and to the controller 28 for data output.
- the arrangement of the sensors 24 preferably enables the sensors 24 to operate as a sensor array 34 which identifies a particular direction of sensed activity from the device 20 .
- Such sensing can include noise detection, low frequency vibration sensing, heat or infrared sensing, seismic signature sensing, and so on.
- the sensors substantially provide circular or spherical 360 degree coverage around the periphery of the device 20 .
- the rate gyros 26 electrically connect to the power supply 32 for power, and to the controller 28 for data output.
- the arrangement of the rate gyros 26 preferably enables the rate gyros 26 to carryout angular rate sensing along different axes, i.e., each rate gyro 26 provides a respective signal indicating a rate of rotation for the earth about a respective axis associated with that rate gyro 26 .
- an X-axis rate gyro 26 outputs an X-axis signal indicating a rate of rotation about the X-axis
- a Y-axis rate gyro 26 outputs a Y-axis signal indicating a rate of rotation about the Y-axis
- a Z-axis rate gyro 26 outputs a Z-axis signal indicating a rate of rotation about the Z-axis.
- each rate gyro 26 is a Microelectromechanical Systems (MEMS) technology angular rate sensor.
- MEMS Microelectromechanical Systems
- each rate gyro 26 is a fiber optic technology angular rate sensor.
- each rate gyro 26 is based on a different technology (e.g., pendulous integrating gyro accelerometers (PIGAs), crystal-based angular rate sensors, classic mechanical, combinations thereof, etc.). It should be understood that multiple rate gyros 26 can be used to sense rotation for each axis, or along different or complementary axes for fault tolerance purposes (e.g., redundant sensing).
- the controller 28 is arranged to receive rate gyro signals from the rate gyros 26 .
- Each rate gyro signal indicates a rate of rotation about a respective axis associated with a particular rate gyro 26 .
- the controller 28 is further arranged to perform a vector sum operation based on the rate gyro signals, and generate a direction signal which identifies a direction resulting from performance of the vector summing operation providing magnitude and direction. Accordingly, the controller 28 is capable of identifying a true north vector from the rate gyro signals which identify measured components of the earth's rotation.
- the identified true north vector is capable of being used in conjunction with information provided by the sensors 24 and the communications interface 30 to provide a bearing on sensed activity.
- multiple deployable stationary device 20 are capable of cooperating (e.g., via triangulation) to provide an accurate ground location of the sensed activity. This feature will be explained in further detail shortly.
- the true north vectoring capabilities of the rate gyros 26 enable the device 20 to operate as a simple, low cost, remotely operational gyroscopic compass. With such a capability, the device 20 is well-suited for identifying the North-South axis of any rotating body (e.g., a moon, an asteroid, an artificial body, etc.). Further details will now be provided with reference to FIG. 2 .
- FIG. 2 is a general diagram of a surveillance system 50 which utilizes multiple deployable stationary devices 20 .
- the surveillance system 50 includes a first deployable stationary device 20 ( 1 ) disposed at a first field location 52 ( 1 ), a second deployable stationary device 20 ( 2 ) disposed at a second field location 52 ( 2 ), and a base station 54 .
- Each deployable stationary device 20 is capable of determining its respective location in the field based on transmissions 56 from a Global Positioning System (GPS) 58 .
- GPS Global Positioning System
- the surveillance system 50 is capable of including other deployable stationary devices 20 at other field locations for enhanced activity sensing (e.g., to cover a larger area, to obtain additional input for higher precision and/or reliability, etc.).
- the controller 28 of the deployable stationary device 20 ( 1 ) is arranged to detect the true north direction based on the signals from the rate gyros 26 ( FIG. 1 ) of that device 20 ( 1 ) (see the arrow N( 1 ) in FIG. 2 ).
- the controller 28 of the deployable stationary device 20 ( 2 ) is arranged to detect the true north direction N based on the signals from the rate gyros 26 of the device 20 ( 2 ) (see the arrow N( 2 ) in FIG. 2 ).
- the controller 28 of the deployable stationary device 20 ( 1 ) is arranged to detect activity 60 (e.g., noise, vibration, heat, etc.) at a remote location 52 (R) (i.e., a particular location of interest) based on sensor signals from the sensors 24 of that device 20 ( 1 ) (see the arrow A( 1 )).
- the controller 28 of the deployable stationary device 20 ( 1 ) is arranged to provide a bearing B( 1 ) on the remote location 52 (R) from the perspective of the deployable stationary device 20 ( 1 ).
- This bearing B( 1 ) e.g., 45 degrees from true north
- elevation information is capable of being sensed (e.g., via the sensors 24 ) and used to accomplish mission oriented objectives.
- the controller 28 of the deployable stationary device 20 ( 2 ) is arranged to detect the same activity 56 at the remote location 52 (R) based on sensor signals from the sensors 24 of the device 20 ( 2 ) (see the arrow A( 2 )).
- the controller 28 of the deployable stationary device 20 ( 1 ) is arranged to provide a bearing B( 2 ) on the remote location 52 (R) from the perspective of the deployable stationary device 20 ( 2 ).
- the bearing B( 2 ) (e.g., 330 degrees from true north) is the angular displacement between the true north direction N( 2 ) and the sensed direction A( 2 ) of the particular location of interest 60 as determined by the device 20 ( 2 ).
- the deployable stationary device 20 ( 1 ) is arranged to transmit a device signal 62 ( 1 ) indicating its location 52 ( 1 ) and the bearing B( 1 ) of the activity 60 to the base station 54 .
- the deployable stationary device 20 ( 2 ) is arranged to transmit a device signal 62 ( 2 ) indicating its location 52 ( 2 ) and the bearing B( 2 ) of the activity 60 to the base station 54 .
- the base station 54 receives this information, the base station 54 is able to locate the activity 60 .
- the base station 54 is capable of identifying the location 52 (R) via triangulation and then take action (e.g., further investigate the activity 60 , etc.). Further details will now be provided with reference to FIG. 3 .
- the X-axis rate gyro 26 provides an X-axis signal 80 (X) indicating a rate of rotation about the X-axis
- a Y-axis rate gyro 26 outputs a Y-axis signal 80 (Y) indicating a rate of rotation about the Y-axis
- a Z-axis rate gyro 26 outputs a Z-axis signal 80 (Z) indicating a rate of rotation about the Z-axis, where the X, Y and Z axes are orthogonal to each other.
- a variety of angular rate sensors are suitable for use as the rate gyros 26 such as MEMS-based components, fiber optic components, and crystal-based components.
- the controller 28 of the deployable stationary device 20 ( 1 ) performs a vector sum operation 82 and generates a direction signal 84 which identifies a directional reference with respect to the particular deployable stationary device 20 ( 1 ).
- the direction signal 84 indicates the true north direction, i.e., the North-South earth axis, relative to the device 20 ( 1 ).
- the controller 28 further monitors the outputs of the sensors 24 which are arranged to detect activity around the device 20 ( 1 ).
- the controller 28 receives a set of sensor output signals 86 and identifies activities 60 relative to the device 20 ( 1 ) based on the set of sensor output signals 86 (also see the particular location of interest 60 in FIG. 2 ).
- the controller 28 is arranged to identify a direction of activity (e.g., a direction of a particular noise, vibration, etc.) based on the set of sensor output signals 86 .
- the controller 28 also knows of the location of the device 20 ( 1 ) from a signal 92 .
- the controller 28 is equipped with GPS circuitry to enable the controller 28 to determine its location and then generate the signal 92 , based on GPS signals (also see the GPS signals 56 in FIG. 2 ).
- the controller 28 obtains location information in a different manner (e.g., manually from a field technician, remotely via remote communications, etc.).
- the device 20 ( 1 ) knows its current location and has a bearing on the activity of interest. Accordingly, the device 20 ( 1 ) performs an operation 94 which generates a device signal 96 ( 1 ) containing this information and transmits the device signal 96 ( 1 ) to an external device (e.g., see the device signals 62 ( 1 ), 62 ( 2 ) which are sent to the base station 54 in FIG. 2 ).
- an external device e.g., see the device signals 62 ( 1 ), 62 ( 2 ) which are sent to the base station 54 in FIG. 2 ).
- the external device receives the device signal 96 ( 1 ) and similar signals from other deployable stationary devices 20 .
- another device signal 96 ( 2 ) is available from another device 20 ( 2 ).
- the device signal 96 ( 2 ) includes the current location of the device 20 ( 2 ) and a bearing on the activity of interest from the perspective of the device 20 ( 2 ).
- the external device then performs a triangulation operation 98 (perhaps further based on other device signals) and outputs a signal 100 which precisely identifies the location of the sensed activity. Accordingly, a user of the external device is now capable of acting on the location identified by the signal 100 . Further details will now be provided with reference to FIG. 4 .
- FIG. 4 is a flowchart of a procedure 200 which is performed by the controller 28 of a deployable stationary device 20 to identify a direction reference (e.g., true north).
- the controller 28 receives rate gyro signals 80 from the rate gyros 26 .
- Each rate gyro signal 80 indicates a rate of rotation about a respective axis (e.g., the X-axis, the Y-axis, the Z-axis) associated with a particular rate gyro 26 (also see FIG. 3 ).
- the controller 28 provides a direction signal 84 ( FIG. 3 ) which identifies a direction resulting from performance of the vector sum operation 82 .
- the identified direction is parallel to the earth's spin axis, i.e., the North-South axis.
- the outputted vector is parallel to the spin axis of that body.
- rate gyros 26 utilizes rate gyros 26 .
- the angular rate sensing capabilities of rate gyros 26 generally make the rate gyros 26 insensitive to levelness and magnetic interference. Rather, the rate gyros 26 provide signals along particular sensing axes (X, Y, and Z axes) which, when vector summed, enable identification of the earth's true north direction. Accordingly, there is no need to convert magnetic north data to true north data. Furthermore, influences such as levelness, temperature, local magnetic field disturbances are unlikely to significantly interfere with the operation of the rate gyros 26 .
- the device 20 was described above as belonging to a surveillance system 20 and being configured to provide a bearing on sensed activity from a stationary location by way of example only.
- the rate gyros 26 combine with circuitry of the controller 28 to provide an electronic gyroscopic compass which is capable of identifying the North-South axis of a rotating body (e.g., a moon, an asteroid, an artificial body, etc.).
- a rotating body e.g., a moon, an asteroid, an artificial body, etc.
- such an electronic gyroscopic compass is capable of being implemented as an advantageously simple, inexpensive, remotely operational device (e.g., the compass of a probe).
- the angular rate sensing aspects of such an electronic gyroscopic compass makes the electronic gyroscopic compass resistant to influences that adversely affect conventional electronic magnetic compasses (e.g., susceptibility to temperature and magnetic interference, sensitivity to levelness, and so on).
- angular rate sensing features are capable of being employed on stationary platforms that perform a particular function.
- these features are capable of being used to take a picture or deploy a device or weapon based on bearing versus the platform orientation.
- Such modifications, enhancements and uses are intended to belong to particular embodiments of the invention.
Abstract
Description
Claims (20)
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Application Number | Priority Date | Filing Date | Title |
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US11/777,072 US7845085B2 (en) | 2007-07-12 | 2007-07-12 | Identifying a directional reference using rate gyros oriented along different axes |
PCT/US2008/068815 WO2009009335A1 (en) | 2007-07-12 | 2008-06-30 | Identifying a directional reference using rate gyros oriented along different axes |
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US11/777,072 US7845085B2 (en) | 2007-07-12 | 2007-07-12 | Identifying a directional reference using rate gyros oriented along different axes |
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US20100024230A1 US20100024230A1 (en) | 2010-02-04 |
US7845085B2 true US7845085B2 (en) | 2010-12-07 |
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2007
- 2007-07-12 US US11/777,072 patent/US7845085B2/en active Active
-
2008
- 2008-06-30 WO PCT/US2008/068815 patent/WO2009009335A1/en active Application Filing
Patent Citations (13)
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US3624365A (en) * | 1969-07-18 | 1971-11-30 | Us Navy | Vertical attitude measuring device |
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US4686771A (en) | 1986-08-28 | 1987-08-18 | Allied Corporation | Gyrocompassing apparatus for stationary equipment |
US5345382A (en) * | 1992-05-15 | 1994-09-06 | Zexel Corporation | Calibration method for a relative heading sensor |
US6361507B1 (en) | 1994-06-16 | 2002-03-26 | Massachusetts Institute Of Technology | Inertial orientation tracker having gradual automatic drift compensation for tracking human head and other similarly sized body |
US6643587B2 (en) | 1999-09-16 | 2003-11-04 | Sirf Technology, Inc. | Navigation system and method for tracking the position of an object |
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US20100024230A1 (en) | 2010-02-04 |
WO2009009335A1 (en) | 2009-01-15 |
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